초록 ▼

A method of fabricating a composite vessel encompassing rapid manufacturing that is applicable to composite hydrogen and other gas storage tanks, both for high-pressure cylinders, as well as low-pressure conformal tanks. The process of fabrication includes using a liner, of metal or plastic material

A method of fabricating a composite vessel encompassing rapid manufacturing that is applicable to composite hydrogen and other gas storage tanks, both for high-pressure cylinders, as well as low-pressure conformal tanks. The process of fabrication includes using a liner, of metal or plastic materials, over which a braided or developed preform is wrapped. The dry fiber wrapped liner is placed in a mold and resin injected into the cavity formed between the liner and the mold outer walls. The liner is flooded with heated and/or cooled pressurized fluid thus enabling complete and independent process control from within the liner for both the resin injection and the cure phases. Fiber placement control is determined through combined biaxial and triaxial braid/preform design, and by wrapping at controlled tension onto the supporting liner. Fiber tension control is further enhanced by the methodology of mold loading whereby tensioning forces are enacted during actual load and close. The process may use thermoset or thermoplastic resins and any of a variety of fibrous reinforcements such as carbon, boron, glass, natural, aramid or other fibers.

대표청구항 ▼

1. A process for manufacturing a hollow composite article, the process comprising the steps of: forming a fiber fabric over-wrap comprising tri-axial fibers by over-wrapping a cylindrical liner with dry fiber material;loading the over-wrapped liner into a mold cavity defining an outer shape of the c

1. A process for manufacturing a hollow composite article, the process comprising the steps of: forming a fiber fabric over-wrap comprising tri-axial fibers by over-wrapping a cylindrical liner with dry fiber material;loading the over-wrapped liner into a mold cavity defining an outer shape of the composite article, said loading being coordinated with mold closing around the over-wrapped liner so as to improve tension on the over-wrap and effectively eliminate undesired wrinkling thereof;activating a fluid system to flood the loaded liner with heat transfer fluid at a temperature and pressure optimized for resin injection viscosity and flow control;injecting resin into the mold cavity so as to saturate the over-wrap, said injecting occurring while the flooded heat transfer fluid provides internal support to the liner balancing against resin injection pressure;forming the composite article by switching the fluid system so as to provide a temperature and pressure of heat transfer fluid fully curing the injected resin; andremoving the composite article from the mold cavity. 2. The process of claim 1, wherein said fiber material comprises carbon, boron, glass, natural, or aramid fibers. 3. The process of claim 1, wherein the over-wrap is a braided material. 4. The process of claim 3, wherein the braided material has an added layer stitched in place to develop variable local thickness. 5. The process of claim 1, wherein the over-wrap is a stitched or woven material. 6. The process of claim 1, wherein the over-wrap is a filament wound tow material. 7. The process of claim 1, wherein the over-wrap also comprises bi-axial fibers. 8. The process of claim 7, wherein the liner comprises end contours which are over-wrapped with said bi-axial fibers, and wherein a cylindrical portion of the liner is over-wrapped with said tri-axial fibers. 9. The process of claim 1 wherein the over-wrap comprises uni-directional fibers facilitating application of tension to the over-wrap. 10. The process of claim 1, further comprising conducting said over-wrapping with tension control over said dry fiber material. 11. The process of claim 1, wherein the liner independently supports said over-wrapping of fiber material. 12. The process of claim 1, further comprising pressurizing the liner by an internal fluid during said over-wrapping so as to provide support to said fiber material. 13. The process of claim 1, wherein the liner is placed on a mandrel support during said over-wrapping. 14. The process of claim 1, wherein said injected resin is thermosetting. 15. The process of claim 14, wherein said temperature of flooded heat transfer fluid is set below a reaction initiation temperature of resin components. 16. The process of claim 15, wherein said temperature of heat transfer fluid used for curing provides heat initiating a reaction of resin components, and wherein excess heat generated during exothermic curing of the resin is absorbed back into the heat transfer fluid through the liner. 17. The process of claim 16, further comprising switching the fluid system so as to provide cold heat transfer fluid cooling the fully cured composite article. 18. The process of claim 1, wherein said injected resin is thermoplastic. 19. The process of claim 18, wherein said temperature of flooded heat transfer fluid is set slightly above a melt temperature of the resin. 20. The process of claim 19, wherein said switching provides a cold heat transfer fluid solidifying the resin. 21. The process of claim 1, further comprising applying vibration to the heat transfer fluid using an excitation pulse during said injecting, during said curing, or both. 22. The process of claim 1, wherein the liner is formed from metal. 23. The process of claim 22, wherein the liner is formed by superplastic forming or spin forming. 24. The process of claim 1, wherein the liner is formed from plastic. 25. The process of claim 24, wherein the liner is formed by blow molding or injection molding. 26. The process of claim 24, wherein plastic material of the liner is modified so as to improve thermal conductivity. 27. The process of claim 26, wherein the plastic material incorporates conductive nano-particulates, chain forming additives, and/or carbon nanotubes. 28. The process of claim 1, wherein the liner comprises end connectors. 29. The process of claim 1, wherein the liner comprises two fluid connections, and wherein heat transfer fluid is delivered into the liner using said fluid connections. 30. The process of claim 1, wherein the liner remains as an integral part of the composite article. 31. The process of claim 1, further comprising removing the liner from the composite article by melting or dissolution. 32. The process of claim 1, wherein the composite article is a compressed gas storage tank. 33. The process of claim 1, wherein the composite article is a fluid storage tank. 34. The process of claim 1, wherein said loading is conducted while rotating the over-wrapped liner so as to provide said improved tension.